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Wing Force & Moment Characterization of Flapping Wings for Micro Air Vehicle Application
Virtual Environment for Visualization and Computational Technologies Enabling Autonomous Vehicles
Unsteady Aerodynamics for Micro Air Vehicles (Aerodynamique instable pour micro-vehicules aeriens)
Towards Autonomous Miniature Rotorcrafts in Cluttered Environments for Scene Understanding
Tightly-Coupled INS, GPS, and Imaging Sensors for Precision Geolocation
Three Component Velocity Measurements in the Tip Vortex of a Micro-Air- Vehicle
Small Power: The Role of Micro and Small UAVs in the Future
Simulation Environment for Aerodynamic Analysis and Design of Flapping Wing Micro Air Vehicles
Sensor Testing System for Design of a Quad-Winged Micro Air Vehicle
Risk-Based Computational Prototyping (Briefing Charts)
Reynolds Number Effects on Thrust Coefficients and PIV for Flapping Wing Micro Air Vehicles
Research Institute for Autonomous Precision Guided Systems
Recommended Crew Systems Capabilities for a Mars Ascent Vehicle as a Function of Flight Duration